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GOE 570 AIRFOIL (goe570-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 570 AIRFOIL (goe570-il)
Reynolds number: 1,000,000
Max Cl/Cd: 20.85 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe570-il-1000000.txt
Download as CSV file: xf-goe570-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 570 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.0704   0.05717   0.05209  -0.2303   0.7339   0.0523
 -19.500  -0.0717   0.05480   0.04965  -0.2315   0.7292   0.0529
 -19.250  -0.0677   0.05311   0.04789  -0.2320   0.7248   0.0529
 -19.000  -0.0654   0.05131   0.04601  -0.2325   0.7203   0.0531
 -18.750  -0.0610   0.04960   0.04426  -0.2331   0.7174   0.0532
 -18.500  -0.0568   0.04797   0.04259  -0.2335   0.7143   0.0533
 -18.250  -0.0549   0.04604   0.04060  -0.2343   0.7108   0.0539
 -18.000  -0.0484   0.04481   0.03930  -0.2342   0.7070   0.0537
 -17.750  -0.0446   0.04333   0.03775  -0.2343   0.7030   0.0539
 -17.500  -0.0392   0.04185   0.03622  -0.2346   0.6997   0.0542
 -17.250  -0.0355   0.04030   0.03463  -0.2348   0.6972   0.0544
 -17.000  -0.0272   0.03924   0.03355  -0.2345   0.6943   0.0543
 -16.750  -0.0228   0.03788   0.03213  -0.2344   0.6912   0.0545
 -16.500  -0.0173   0.03670   0.03090  -0.2341   0.6877   0.0547
 -16.250  -0.0117   0.03566   0.02979  -0.2334   0.6837   0.0547
 -16.000  -0.0039   0.03461   0.02868  -0.2331   0.6801   0.0547
 -15.750   0.0017   0.03347   0.02753  -0.2326   0.6779   0.0548
 -15.500   0.0075   0.03243   0.02647  -0.2318   0.6748   0.0549
 -15.250   0.0119   0.03138   0.02538  -0.2308   0.6716   0.0551
 -15.000   0.0161   0.03042   0.02437  -0.2296   0.6681   0.0552
 -14.750   0.0203   0.02953   0.02343  -0.2283   0.6644   0.0552
 -14.500   0.0221   0.02853   0.02237  -0.2268   0.6602   0.0554
 -14.250   0.0221   0.02741   0.02124  -0.2251   0.6580   0.0557
 -14.000   0.0222   0.02633   0.02016  -0.2233   0.6552   0.0561
 -13.750   0.0235   0.02543   0.01923  -0.2214   0.6515   0.0562
 -13.500   0.0199   0.02457   0.01832  -0.2185   0.6474   0.0564
 -13.250   0.0160   0.02386   0.01755  -0.2153   0.6429   0.0564
 -13.000   0.0136   0.02305   0.01671  -0.2124   0.6393   0.0565
 -12.750   0.0129   0.02229   0.01594  -0.2097   0.6363   0.0568
 -12.500   0.0136   0.02167   0.01530  -0.2069   0.6323   0.0572
 -12.250   0.0102   0.02105   0.01463  -0.2033   0.6279   0.0571
 -12.000   0.0050   0.02052   0.01404  -0.1992   0.6232   0.0573
 -11.750   0.0041   0.02002   0.01351  -0.1957   0.6193   0.0574
 -11.500   0.0040   0.01957   0.01304  -0.1922   0.6151   0.0578
 -11.250  -0.0018   0.01918   0.01262  -0.1875   0.6102   0.0579
 -11.000  -0.0113   0.01890   0.01227  -0.1819   0.6052   0.0581
 -10.750  -0.0166   0.01859   0.01192  -0.1770   0.6008   0.0582
 -10.500  -0.0164   0.01830   0.01161  -0.1730   0.5967   0.0584
 -10.250  -0.0206   0.01805   0.01132  -0.1680   0.5918   0.0585
 -10.000  -0.0291   0.01793   0.01115  -0.1621   0.5864   0.0588
  -9.750  -0.0371   0.01777   0.01095  -0.1563   0.5818   0.0590
  -9.500  -0.0375   0.01759   0.01075  -0.1518   0.5775   0.0593
  -9.250  -0.0437   0.01748   0.01059  -0.1462   0.5722   0.0593
  -9.000  -0.0540   0.01746   0.01052  -0.1397   0.5671   0.0595
  -8.750  -0.0576   0.01739   0.01040  -0.1344   0.5629   0.0598
  -8.500  -0.0598   0.01731   0.01030  -0.1294   0.5587   0.0600
  -8.250  -0.0650   0.01728   0.01024  -0.1237   0.5545   0.0601
  -8.000  -0.0717   0.01731   0.01021  -0.1178   0.5499   0.0603
  -7.750  -0.0803   0.01740   0.01025  -0.1115   0.5453   0.0605
  -7.500  -0.0771   0.01736   0.01020  -0.1073   0.5423   0.0607
  -7.250  -0.0761   0.01739   0.01020  -0.1027   0.5384   0.0608
  -7.000  -0.0802   0.01740   0.01017  -0.0973   0.5346   0.0612
  -6.750  -0.0856   0.01747   0.01019  -0.0916   0.5298   0.0617
  -6.500  -0.0869   0.01753   0.01022  -0.0867   0.5262   0.0622
  -6.250  -0.0808   0.01751   0.01020  -0.0830   0.5235   0.0628
  -6.000  -0.0754   0.01753   0.01020  -0.0792   0.5201   0.0634
  -5.750  -0.0724   0.01765   0.01030  -0.0751   0.5167   0.0638
  -5.500  -0.0706   0.01782   0.01043  -0.0708   0.5129   0.0640
  -5.250  -0.0669   0.01799   0.01055  -0.0668   0.5085   0.0649
  -5.000  -0.0564   0.01803   0.01060  -0.0640   0.5061   0.0655
  -4.750  -0.0474   0.01814   0.01070  -0.0610   0.5035   0.0661
  -4.500  -0.0375   0.01827   0.01081  -0.0582   0.5005   0.0664
  -4.250  -0.0280   0.01843   0.01093  -0.0553   0.4974   0.0674
  -4.000  -0.0228   0.01865   0.01112  -0.0518   0.4935   0.0687
  -3.750  -0.0130   0.01883   0.01128  -0.0491   0.4901   0.0697
  -3.500   0.0025   0.01891   0.01139  -0.0474   0.4882   0.0718
  -3.250   0.0185   0.01902   0.01151  -0.0458   0.4859   0.0735
  -3.000   0.0340   0.01914   0.01164  -0.0442   0.4832   0.0765
  -2.750   0.0454   0.01941   0.01191  -0.0420   0.4798   0.0795
  -2.500   0.0573   0.01969   0.01219  -0.0399   0.4765   0.0833
  -2.250   0.0712   0.01990   0.01240  -0.0382   0.4725   0.0918
  -2.000   0.0903   0.02001   0.01257  -0.0373   0.4708   0.1008
  -1.750   0.1081   0.02015   0.01279  -0.0364   0.4687   0.1147
  -1.500   0.1276   0.02012   0.01302  -0.0359   0.4665   0.1651
  -1.250   0.1450   0.02040   0.01336  -0.0349   0.4637   0.1810
  -1.000   0.1613   0.02074   0.01371  -0.0338   0.4608   0.1891
  -0.750   0.1736   0.02124   0.01420  -0.0321   0.4573   0.1946
  -0.500   0.1896   0.02165   0.01456  -0.0309   0.4540   0.1983
  -0.250   0.2089   0.02194   0.01489  -0.0304   0.4523   0.2032
   0.000   0.2287   0.02223   0.01522  -0.0299   0.4504   0.2085
   0.250   0.2469   0.02260   0.01559  -0.0292   0.4480   0.2115
   0.500   0.2622   0.02310   0.01608  -0.0281   0.4453   0.2138
   0.750   0.2779   0.02359   0.01654  -0.0271   0.4428   0.2156
   1.000   0.2924   0.02411   0.01703  -0.0260   0.4395   0.2192
   1.250   0.3110   0.02446   0.01737  -0.0254   0.4364   0.2244
   1.500   0.3278   0.02496   0.01792  -0.0247   0.4348   0.2282
   1.750   0.3458   0.02541   0.01840  -0.0242   0.4328   0.2320
   2.000   0.3640   0.02588   0.01886  -0.0237   0.4305   0.2351
   2.250   0.3825   0.02629   0.01932  -0.0234   0.4283   0.2452
   2.500   0.3974   0.02690   0.01992  -0.0225   0.4258   0.2486
   2.750   0.4112   0.02753   0.02061  -0.0216   0.4229   0.2683
   3.000   0.4324   0.02764   0.02111  -0.0220   0.4196   0.3800
   3.250   0.4507   0.02808   0.02175  -0.0218   0.4183   0.4244
   3.500   0.4691   0.02854   0.02232  -0.0215   0.4167   0.4553
   3.750   0.4861   0.02907   0.02294  -0.0210   0.4148   0.4757
   4.000   0.5007   0.02974   0.02369  -0.0203   0.4126   0.4962
   4.250   0.5151   0.03040   0.02441  -0.0196   0.4099   0.5183
   4.500   0.5290   0.03103   0.02513  -0.0188   0.4073   0.5478
   4.750   0.5437   0.03159   0.02576  -0.0180   0.4043   0.5759
   5.000   0.5604   0.03193   0.02627  -0.0174   0.4023   0.6227
   5.250   0.5669   0.03250   0.02721  -0.0152   0.4009   0.7084
   5.500   0.7344   0.03528   0.03081  -0.0463   0.3988   0.9405
   5.750   0.7266   0.03603   0.03157  -0.0411   0.3966   0.9533
   6.000   0.7517   0.03710   0.03262  -0.0427   0.3944   0.9588
   6.250   0.7741   0.03833   0.03382  -0.0440   0.3917   0.9647
   6.500   0.7791   0.03934   0.03480  -0.0416   0.3893   0.9700
   6.750   0.7989   0.04019   0.03559  -0.0419   0.3862   0.9731
   7.000   0.8407   0.04172   0.03715  -0.0476   0.3850   0.9750
   7.250   0.8855   0.04313   0.03856  -0.0537   0.3834   0.9776
   7.500   0.9217   0.04440   0.03984  -0.0580   0.3815   0.9803
   7.750   0.9490   0.04553   0.04096  -0.0604   0.3796   0.9826
   8.000   0.9749   0.04676   0.04218  -0.0626   0.3776   0.9855
   8.250   0.9867   0.04829   0.04370  -0.0625   0.3752   0.9876
   8.500   1.0085   0.04970   0.04508  -0.0641   0.3727   0.9900
   8.750   1.0441   0.05044   0.04577  -0.0680   0.3699   0.9916
   9.000   1.0676   0.05173   0.04710  -0.0703   0.3686   0.9931
   9.250   1.0953   0.05290   0.04829  -0.0731   0.3672   0.9953
   9.500   1.1194   0.05429   0.04969  -0.0756   0.3653   0.9974
   9.750   1.1452   0.05577   0.05119  -0.0785   0.3635   0.9994
  10.000   1.1595   0.05699   0.05241  -0.0788   0.3615   0.9998
  10.250   1.1698   0.05822   0.05362  -0.0784   0.3593   1.0000
  10.500   1.1784   0.05935   0.05473  -0.0776   0.3569   1.0000
  10.750   1.1938   0.05991   0.05524  -0.0773   0.3544   1.0000
  11.000   1.1985   0.06144   0.05681  -0.0763   0.3532   1.0000
  11.250   1.2058   0.06278   0.05820  -0.0756   0.3519   1.0000
  11.500   1.2148   0.06399   0.05943  -0.0750   0.3504   1.0000
  11.750   1.2229   0.06529   0.06075  -0.0743   0.3489   1.0000
  12.000   1.2269   0.06693   0.06241  -0.0733   0.3469   1.0000
  12.250   1.2348   0.06823   0.06371  -0.0727   0.3451   1.0000
  12.500   1.2437   0.06944   0.06492  -0.0722   0.3433   1.0000
  12.750   1.2544   0.07047   0.06592  -0.0718   0.3412   1.0000
  13.000   1.2727   0.07081   0.06622  -0.0720   0.3388   1.0000
  13.250   1.2719   0.07293   0.06840  -0.0709   0.3375   1.0000
  13.500   1.2776   0.07447   0.06999  -0.0703   0.3364   1.0000
  13.750   1.2829   0.07606   0.07161  -0.0697   0.3347   1.0000
  14.000   1.2859   0.07787   0.07345  -0.0689   0.3328   1.0000
  14.250   1.2891   0.07965   0.07526  -0.0682   0.3310   1.0000
  14.500   1.2978   0.08093   0.07655  -0.0679   0.3295   1.0000
  14.750   1.3066   0.08216   0.07777  -0.0676   0.3277   1.0000
  15.000   1.3198   0.08298   0.07856  -0.0676   0.3257   1.0000
  15.250   1.3381   0.08329   0.07885  -0.0680   0.3241   1.0000
  15.500   1.3385   0.08533   0.08094  -0.0672   0.3226   1.0000
  15.750   1.3368   0.08758   0.08325  -0.0663   0.3213   1.0000
  16.000   1.3307   0.09029   0.08603  -0.0652   0.3183   1.0000
  16.250   1.3317   0.09228   0.08806  -0.0646   0.3169   1.0000
  16.500   1.3342   0.09417   0.08996  -0.0641   0.3146   1.0000
  16.750   1.3417   0.09553   0.09129  -0.0639   0.3122   1.0000
  17.000   1.3580   0.09599   0.09171  -0.0643   0.3097   1.0000
  17.250   1.3739   0.09649   0.09220  -0.0646   0.3085   1.0000
  17.500   1.3620   0.09975   0.09557  -0.0633   0.3072   1.0000
  17.750   1.3545   0.10260   0.09849  -0.0624   0.3049   1.0000
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